2016
DOI: 10.2298/tsci150914208z
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Experimental and simulation testing of thermal loading in the jet tabs of a thrust vector control system

Abstract: The paper discusses the temperature changes in mechanical jet tabs in a system of rocket motor thrust vector control, estimated by the simulation and experimental tests methodology. The heat transfer calculation is based on complex computational fluid dynamics simulations of both the nozzle and external tab flows, as the comprehensive integral flow zones with high flow parameters gradients. Due to a complexity of the model for flow calculations, the experimental estimation of the calculated r… Show more

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Cited by 4 publications
(4 citation statements)
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“…The radiation model for the numerical simulation was P-1. More about this model can be found in [16]. Experimental results were obtained by firing on proving ground with a 20mm gun which is shown in figure 3.…”
Section: Numerical Modelmentioning
confidence: 99%
“…The radiation model for the numerical simulation was P-1. More about this model can be found in [16]. Experimental results were obtained by firing on proving ground with a 20mm gun which is shown in figure 3.…”
Section: Numerical Modelmentioning
confidence: 99%
“…The convective heat transfer coefficient is calculated from turbulent boundary layer and the P-1 heat radiation model is applied. More details are given in [25].…”
Section: The Nern Code Calculationmentioning
confidence: 99%
“…Fuel combustion can produce a significant thermal effect on the total load level. Detailed CFD analysis of the thermal effect at the rocket nozzle is analyzed in Zivkovic et al 6 Jet tabs of the nozzle for rocket flight control are significantly thermally loaded. Temperature distribution and heat transfer are identified in order to find out the solution to prevent material degradation of nozzle tabs.…”
Section: Introductionmentioning
confidence: 99%